2 0 0 0 OA BADAモデルを用いた旅客機の軌道最適化による運航効率の評価
- 著者
- 宮本 侑斗 原田 明徳 ビクラマシンハ ナヴィンダ キトマル 宮沢 与和 船曳 孝三
- 出版者
- 一般社団法人 日本航空宇宙学会
- 雑誌
- 航空宇宙技術 (ISSN:18840477)
- 巻号頁・発行日
- vol.13, pp.1-10, 2014 (Released:2014-02-13)
- 参考文献数
- 11
- 被引用文献数
- 3 7
Fuel efficient flight is demanded due to air traffic increase, environmental concerns and skyrocketing fuel prices. To achieve an effective futuristic air traffic management system, realization of TBO (Trajectory Based Operations) optimized from departure to arrival is aimed in CARATS (Collaborative Actions for Renovation of Air Traffic Systems). In this paper, 4-D trajectory of passenger aircraft is optimized for fuel minimization on the assumption that aircraft is not bounded by any air traffic control constraints. BADA (Base of Aircraft Data) model is adopted for aircraft performance model, and dynamic programming is used to calculate the optimal trajectory. The optimal trajectory is compared with airliner’s flight trajectory by evaluating fuel consumption, flight time and flight range. Examples show that considerable amounts of reduction in fuel consumption could be achieved by trajectory optimization compared to the estimated values of actual flights.
1 0 0 0 到着時刻を指定した旅客機の軌道最適化
- 著者
- 宮沢 与和 ビクラマシンハ ナビィンダ キトマル 原田 明徳 宮本 侑斗
- 出版者
- 一般社団法人 日本航空宇宙学会
- 雑誌
- 航空宇宙技術 (ISSN:18840477)
- 巻号頁・発行日
- vol.12, pp.31-38, 2013 (Released:2013-03-06)
- 参考文献数
- 10
- 被引用文献数
- 3 6 2
In the future air transportation system, airspace will be efficiently used and each aircraft can optimize its own performance. Due to limited capacity of the airspace like terminal area, however, some sort of adjustment for each aircraft is necessary to maintain separation among multiple aircraft. Fixed arrival time is a basic solution to the problem. This paper studies the effect of arrival time assignment on the performance by assuming that each aircraft generates its own flight plan by minimizing its fuel consumption. Dynamic programming trajectory optimization is used to calculate the optimal flight profile composed of altitude and velocity. The result shows that the arrival time adjustment is efficiently performed in the descent phase, if the required amount of time to be adjusted is not large.
1 0 0 0 OA 多数遅れモデル/多数設計点法によるロバスト飛行制御系の設計
- 著者
- 宮沢 与和
- 出版者
- 一般社団法人 日本航空宇宙学会
- 雑誌
- 日本航空宇宙学会誌 (ISSN:00214663)
- 巻号頁・発行日
- vol.41, no.473, pp.318-323, 1993-06-05 (Released:2010-12-16)
- 参考文献数
- 10
- 被引用文献数
- 1 2